Numerical Analysis of Supersonic Jet Flow from Vertical Landing Rocket Vehicle in Landing Phase
Toshiyuki Suzukia; Satoshi Nonakab; Yoshifumi Inatanib a Institute of Aerospace Technology, JAXA 7-44-1 Jindaiji-Higashi-machi, Chofu, Tokyo 182-8522, Japanb Institute of Space and Astronautical Science, JAXA 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan
Keywords
Large Eddy Simulation
Opposing Jet
1 INTRODUCTION
As a future space transportation system, a working group at Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA) proposed a concept of a fully reusable launch vehicle.1 The proposed vehicle is a single stage vertical taking off and landing (VTOL) type one. For the purpose of verification of ...
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